FR3035676B1 - Aube munie de plateformes possedant un raidisseur - Google Patents
Aube munie de plateformes possedant un raidisseurInfo
- Publication number
- FR3035676B1 FR3035676B1 FR1553849A FR1553849A FR3035676B1 FR 3035676 B1 FR3035676 B1 FR 3035676B1 FR 1553849 A FR1553849 A FR 1553849A FR 1553849 A FR1553849 A FR 1553849A FR 3035676 B1 FR3035676 B1 FR 3035676B1
- Authority
- FR
- France
- Prior art keywords
- dawn
- stiffener
- possessing
- platforms
- platforms possessing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 239000003351 stiffener Substances 0.000 title 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B11/00—Making preforms
- B29B11/06—Making preforms by moulding the material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B11/00—Making preforms
- B29B11/14—Making preforms characterised by structure or composition
- B29B11/16—Making preforms characterised by structure or composition comprising fillers or reinforcement
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
- B29C45/02—Transfer moulding, i.e. transferring the required volume of moulding material by a plunger from a "shot" cavity into a mould cavity
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
- B29C45/14—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles
- B29C45/1418—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles the inserts being deformed or preformed, e.g. by the injection pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/26—Antivibration means not restricted to blade form or construction or to blade-to-blade connections or to the use of particular materials
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
- B29C45/14—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles
- B29C45/1418—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles the inserts being deformed or preformed, e.g. by the injection pressure
- B29C2045/14237—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles the inserts being deformed or preformed, e.g. by the injection pressure the inserts being deformed or preformed outside the mould or mould cavity
- B29C2045/14245—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles the inserts being deformed or preformed, e.g. by the injection pressure the inserts being deformed or preformed outside the mould or mould cavity using deforming or preforming means outside the mould cavity
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2063/00—Use of EP, i.e. epoxy resins or derivatives thereof, as moulding material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
- B29K2105/20—Inserts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
- B29L2031/082—Blades, e.g. for helicopters
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/80—Platforms for stationary or moving blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Manufacturing & Machinery (AREA)
- Composite Materials (AREA)
- Architecture (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Moulding By Coating Moulds (AREA)
- Woven Fabrics (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Reinforced Plastic Materials (AREA)
Priority Applications (9)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1553849A FR3035676B1 (fr) | 2015-04-29 | 2015-04-29 | Aube munie de plateformes possedant un raidisseur |
CA2984127A CA2984127C (fr) | 2015-04-29 | 2016-04-26 | Aube munie de plateformes possedant un raidisseur |
BR112017023307-0A BR112017023307B1 (pt) | 2015-04-29 | 2016-04-26 | Pré-forma, pá, roda de pás, e, motor de turbina |
EP16722311.4A EP3288736B1 (fr) | 2015-04-29 | 2016-04-26 | Aube munie de plateformes possedant un raidisseur |
CN201680024880.3A CN107548428B (zh) | 2015-04-29 | 2016-04-26 | 包括带有加固件的平台的叶片 |
US15/569,665 US10519776B2 (en) | 2015-04-29 | 2016-04-26 | Blade comprising lands with a stiffener |
RU2017141349A RU2699649C2 (ru) | 2015-04-29 | 2016-04-26 | Лопатка, оснащенная полками, имеющими элемент жесткости |
JP2017556595A JP6816022B2 (ja) | 2015-04-29 | 2016-04-26 | 補強材を含むランドを備えるブレード |
PCT/FR2016/050979 WO2016174343A1 (fr) | 2015-04-29 | 2016-04-26 | Aube munie de plateformes possedant un raidisseur |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1553849A FR3035676B1 (fr) | 2015-04-29 | 2015-04-29 | Aube munie de plateformes possedant un raidisseur |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3035676A1 FR3035676A1 (fr) | 2016-11-04 |
FR3035676B1 true FR3035676B1 (fr) | 2017-05-12 |
Family
ID=53484037
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1553849A Active FR3035676B1 (fr) | 2015-04-29 | 2015-04-29 | Aube munie de plateformes possedant un raidisseur |
Country Status (9)
Country | Link |
---|---|
US (1) | US10519776B2 (fr) |
EP (1) | EP3288736B1 (fr) |
JP (1) | JP6816022B2 (fr) |
CN (1) | CN107548428B (fr) |
BR (1) | BR112017023307B1 (fr) |
CA (1) | CA2984127C (fr) |
FR (1) | FR3035676B1 (fr) |
RU (1) | RU2699649C2 (fr) |
WO (1) | WO2016174343A1 (fr) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3035675B1 (fr) * | 2015-04-29 | 2017-05-12 | Snecma | Aube munie de plateformes comportant des inserts |
FR3063448B1 (fr) * | 2017-03-01 | 2019-04-05 | Safran Aircraft Engines | Preforme et aube monobloc pour turbomachine |
US10738630B2 (en) * | 2018-02-19 | 2020-08-11 | General Electric Company | Platform apparatus for propulsion rotor |
FR3089844B1 (fr) * | 2018-12-13 | 2022-02-18 | Safran Aircraft Engines | Préforme fibreuse d’une pièce de turbomachine |
FR3100471B1 (fr) * | 2019-09-10 | 2022-12-09 | Safran Aircraft Engines | Préforme pour aube composite |
FR3102392B1 (fr) * | 2019-10-29 | 2021-10-08 | Safran | Préforme fibreuse tissée pour réaliser une aube de soufflante en matériau composite |
FR3107915B1 (fr) * | 2020-03-03 | 2022-02-04 | Safran Aircraft Engines | Procede de fabrication d’une plateforme composite pour une soufflante de turbomachine d’aeronef |
US11834960B2 (en) | 2022-02-18 | 2023-12-05 | General Electric Company | Methods and apparatus to reduce deflection of an airfoil |
US12078080B1 (en) | 2023-04-21 | 2024-09-03 | General Electric Company | Airfoil assembly with a trunnion and spar |
US11846192B1 (en) | 2023-04-21 | 2023-12-19 | General Electric Company | Airfoil assembly with a trunnion and spar |
Family Cites Families (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4589176A (en) * | 1983-11-25 | 1986-05-20 | Rockwell International Corporation | Fiber-composite turbine blade and method for its construction |
JP3831265B2 (ja) * | 2002-01-21 | 2006-10-11 | 本田技研工業株式会社 | 静翼構造体の製造方法 |
RU2311536C2 (ru) * | 2003-06-10 | 2007-11-27 | Исикавадзима-Харима Хэви Индастриз Ко., Лтд. | Компонент турбинного двигателя (варианты) и способ изготовления поверхностно обработанного компонента турбинного двигателя (варианты) |
RU2320464C2 (ru) * | 2003-06-11 | 2008-03-27 | Исикавадзима-Харима Хэви Индастриз Ко., Лтд. | Способ восстановления компонента машины, способ изготовления восстановленного компонента машины, способ изготовления компонента машины, газотурбинный двигатель, электроэрозионный станок, способ восстановления компонента турбины и способ изготовления восстановленного компонента турбины |
RU2350757C1 (ru) * | 2007-09-21 | 2009-03-27 | Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" | Композиционная лопатка турбомашины |
US8142163B1 (en) * | 2008-02-01 | 2012-03-27 | Florida Turbine Technologies, Inc. | Turbine blade with spar and shell |
JP5550370B2 (ja) * | 2010-02-05 | 2014-07-16 | 本田技研工業株式会社 | 航空機翼構造の製造方法 |
FR2963381B1 (fr) * | 2010-07-27 | 2015-04-10 | Snecma | Etancheite inter-aubes pour une roue de turbine ou de compresseur de turbomachine |
FR2975734B1 (fr) * | 2011-05-27 | 2013-05-31 | Snecma | Procede de renforcement d'une piece mecanique de turbomachine |
FR2981979B1 (fr) * | 2011-10-28 | 2013-11-29 | Snecma | Roue de turbine pour une turbomachine |
FR2983428B1 (fr) * | 2011-12-01 | 2014-01-17 | Snecma Propulsion Solide | Procede de fabrication d'une aube de turbomachine en materiau composite a plates-formes integrees |
CA2862685C (fr) * | 2012-01-09 | 2020-03-10 | Snecma | Preforme fibreuse d'une aube de turbomachine en materiau composite a plate-forme integree, et son procede de realisation |
FR2987086B1 (fr) * | 2012-02-22 | 2014-03-21 | Snecma | Joint lineaire de plateforme inter-aubes |
FR2989977B1 (fr) * | 2012-04-26 | 2014-05-23 | Snecma | Ebauche fibreuse tissee en une seule piece par tissage tridimensionnel pour la realisation d'une plate-forme a caisson ferme pour soufflante de turbomachine en materiau composite |
FR2989991B1 (fr) * | 2012-04-30 | 2016-01-08 | Snecma | Renfort structurel metallique d'aube de turbomachine |
US9017033B2 (en) * | 2012-06-07 | 2015-04-28 | United Technologies Corporation | Fan blade platform |
WO2014076408A1 (fr) * | 2012-11-13 | 2014-05-22 | Snecma | Preforme et aube monobloc pour turbomachine |
US10047625B2 (en) * | 2013-03-15 | 2018-08-14 | United Technologies Corporation | Fan blade root integrated sealing solution |
US10202853B2 (en) * | 2013-09-11 | 2019-02-12 | General Electric Company | Ply architecture for integral platform and damper retaining features in CMC turbine blades |
FR3037097B1 (fr) * | 2015-06-03 | 2017-06-23 | Snecma | Aube composite comprenant une plateforme munie d'un raidisseur |
FR3035677B1 (fr) * | 2015-04-29 | 2017-05-12 | Snecma | Aube munie de plateformes possedant des portions d'accrochage |
US10577939B2 (en) * | 2016-11-01 | 2020-03-03 | Rolls-Royce Corporation | Turbine blade with three-dimensional CMC construction elements |
US10392946B2 (en) * | 2016-12-21 | 2019-08-27 | Rolls-Royce North American Technologies Inc. | Turbine blade with reinforced platform for composite material construction |
US10731479B2 (en) * | 2017-01-03 | 2020-08-04 | Raytheon Technologies Corporation | Blade platform with damper restraint |
-
2015
- 2015-04-29 FR FR1553849A patent/FR3035676B1/fr active Active
-
2016
- 2016-04-26 CA CA2984127A patent/CA2984127C/fr active Active
- 2016-04-26 BR BR112017023307-0A patent/BR112017023307B1/pt active IP Right Grant
- 2016-04-26 JP JP2017556595A patent/JP6816022B2/ja active Active
- 2016-04-26 US US15/569,665 patent/US10519776B2/en active Active
- 2016-04-26 CN CN201680024880.3A patent/CN107548428B/zh active Active
- 2016-04-26 EP EP16722311.4A patent/EP3288736B1/fr active Active
- 2016-04-26 RU RU2017141349A patent/RU2699649C2/ru active
- 2016-04-26 WO PCT/FR2016/050979 patent/WO2016174343A1/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
JP6816022B2 (ja) | 2021-01-20 |
US10519776B2 (en) | 2019-12-31 |
RU2017141349A (ru) | 2019-05-29 |
FR3035676A1 (fr) | 2016-11-04 |
US20180119550A1 (en) | 2018-05-03 |
EP3288736B1 (fr) | 2019-03-13 |
CN107548428A (zh) | 2018-01-05 |
BR112017023307A2 (pt) | 2018-08-14 |
RU2699649C2 (ru) | 2019-09-06 |
WO2016174343A1 (fr) | 2016-11-03 |
CA2984127A1 (fr) | 2016-11-03 |
RU2017141349A3 (fr) | 2019-07-26 |
BR112017023307B1 (pt) | 2022-04-19 |
CN107548428B (zh) | 2019-12-17 |
EP3288736A1 (fr) | 2018-03-07 |
CA2984127C (fr) | 2023-01-10 |
JP2018523040A (ja) | 2018-08-16 |
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Legal Events
Date | Code | Title | Description |
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